1. Airborne Science Program ISPRS / Canadian Geomatics Conference June 14 – 18, 2010 Jeff Myers Carl Sorenson Univ. of California, Santa Cruz NASA Ames Research Center Developing Airborne Sensor and Data Network Interface Standards

2. WG-I TOR 2 Goal: “Develop airborne sensor interface format standards, in coordination with other working groups, to promote maximum sensor portability between aircraft, and increasing science yield from the sensors”

3. Basic Factors for Instrument Portability 1.Mechanical Accommodation (mounts, windows, ports, antennas, inlets, etc.) - Airworthiness certification - Safety (active systems, gas bottles, etc.) 2.Electrical power (28V DC, 110V/440Hz AC) - Connectors & polarity - Hard-wired controls 3. Data communications: - From aircraft to sensor - From sensor to aircraft (& beyond)

4. Instrument Portability: Data Communication Requirements Data from aircraft to sensor: - Command and control - Aircraft state data (navigation, met data, etc.) (RS-232,-422, ARINC-429,-1553, Synchro, etc) - GPS antenna feeds (L1/L2, OmniStar, etc. Data from sensor to aircraft (& beyond) - System health and status, engineering data - Science data (high and low rate content) Most requirements can be satisfied via a single Ethernet connection (may include AIRINC-664 for low-latency state data) Common data formats are essential

5. Common Data Formats: The IWGADTS* IWG1 Standard Packet It is designed to provide a common aircraft housekeeping data format to replace all the various legacy formats on the different science aircraft. The Interagency Working Group Standard Format Number 1 (IWG1) is a simple ASCII CSV format which is transmitted as a UDP packet at 1 Hz. Currently in use on the NASA and NSF/NCAR platforms. Example Packet: “IWG1,yyyymmddThhmmss,value,value,value,,value\r\n” http://www.eol.ucar.edu/raf/Software/iwgadts/IWG1_Def.html *Intergovernmental Working Group for Airborne Data and Telemetry Standards

6. Enabling Standards: Instrument Communication Formats From Aircraft: - IWG1 Standard housekeeping data broadcast (ASCII CSV) --- - International Standard Port 7071 Ex: “IWG1, Timestamp, std aircraft state parameters, + as needed” http://www.eol.ucar.edu/raf/Software/iwgadts/IWG1_Def.html From Instrument: -Instrument status and low-rate data CSV packets (1 Hz broadcast by instrument) Ex: “Instrument identifier, time stamp, status code, up to 16 parms” -Arbitrary data packet (Bidirectional, port-to-port)

7. Example Implementation: RQ4-A Global Hawk Payload Support Infrastructure Payload communication on the NASA Global Hawk aircraft is implemented using an airborne 100-T Ethernet network with a port for each instrument Network services include: Housekeeping data broadcast Bi-directional sat-com connections Payload status monitoring Shared mass data storage GIS database server Time synchronization Uses IWGADTS standards

8. Global Hawk UAS Payload Communications & Control System Payload Instruments Network Host Link Module (Database & Telemetry I/O) GHOC Link Server Experimenter Workstations Web-Based Users Master Payload Control System & PDU Pilot’s MPCS GUI Instrument Power & Control Ethernet Global Hawk Ground Operations Center AIRCRAFT GROUND PI Hardware Aircraft HW Iridium (4 ch)Iridium (2 ch)Ku-Band Sat-Com Flight Deck Interface Panels (8) Visualization Tools

9. The Real-Time Airborne Science Data Network Architecture Airborne Science Web Portal Provides: Science Data Bases, CDE, OGC Web Services, KML Generators, Data Visualization Tools DFRC GHOC Web-Based Mission Participants DC-8, P-3, ER-2, WB-57B200, Small UASGlobal Hawk, Ikhana Portable Ground Stations Satellite Products Model Inputs Sensor Webs INMARSAT-BGAN & Iridium Sat-Com Ku-Band & Iridium Sat-Com

10. Instrument Power & Control Interfaces AC Circuit #2 AC Circuit #1 DC Circuit #2 DC Circuit #1 Safety Interlock Circuit IRIG-B (coax insert) GPS (coax insert) The New NASA Standard Experimenter Interface Panel (Intended for Global Hawk, ER-2, WB-57, and others) Available Signals: Two (2) sets of 3ф, 400Hz AC (Phases A,B,C + Neutral; 10 Amps/phase) Two (2) sets of 28VDC power + return (15 Amps ea.) Safety Interlock circuit – both contacts of a normally open relay GPS (L1/L2 Omnistar) IRIG-B Experimenter Interface Panel (EIP) Connector: D38999/20WG- 16SN (16x AWG #16)

11. Instrument Ethernet Data Interfaces Ethernet Connectors – Two Types Amphenol D38999/III Quadrax ARINC-664 recommendation Very high reliability, more expensive One insert for 100Mbit, two for Gig-E Amphenol PCD RJ Field – RJ45 in 38999 Shell Less reliability, cheaper Recommendation: Quadrax for permanent installation on the plane (Server, EIP, feed- throughs, etc.) Instruments have option of Quadrax or RJ45 Field; use adapters as needed QuadraxRJ45 Field Airborne Ethernet Switch Network Host (REVEAL/NASDAT)

12. Summary The aircraft network is a standard Ethernet TCP/IP LAN with 10/100T ports. Instruments are required to include an Ethernet interface and to provide a simple Comma Separated Value (CSV) status packet Connections to the switches are made with standard RJ45 or ruggedized RJ45 connectors Instruments are required to implement Universal Time Code synchronization via Network Time Protocol (NTP), IRIG-B, or GPS signal. Routing of any direct connections to the ground via the wide band satcom link, when available, is done using Network Address Translation (NAT) using the aircraft router

13. Towards an Integrated Sensor Web for Environmental Observation Courtesy MBARI